Helicopter control system based on Simulink

Catalog

1. Algorithm description

2. Partial procedure

3. Preview of some simulation drawings

4. Source code acquisition method  

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1. Algorithm description

        Helicopter body vibration reduction is the goal , The feedforward control problem based on adaptive filtering technology is studied . In order to simulate the mechanical characteristics of the airframe and the excitation effect of the rotor on the airframe , Adopted FIR,SIIR Wait for the filter model to identify and control . Through the simulation of the actuator and the corresponding filtering algorithm , The convergence and convergence speed of the algorithm are suggested . Due to the coupling characteristics and model uncertainties of helicopters , Make its control more complicated , This makes the research of its controller design very necessary . The robust control of helicopter is studied . The nonlinear modeling of wing helicopter is carried out according to the dynamic equation , In order to facilitate the design of loop forming controller, the model is linearized ; stay Simulink Nonlinear model and simulation control system are built in .

2. Partial procedure

3. Preview of some simulation drawings

 

 

 

 

 

4. Source code acquisition method  

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be based on simulink Helicopter control system based on + Program operation video

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